Modeling of Dual-Spinning Projectile with Canard and Trajectory Filtering
The article establishes a seven-degree-of-freedom projectile trajectory model for a new type of spinning projectile. Based on this model, a numerical analysis is performed on the ballistic characteristics of the projectile, and the trajectory of the dual-spinning projectile is filtered with the unsc...
Saved in:
| Main Authors: | , |
|---|---|
| Format: | Article |
| Language: | English |
| Published: |
Wiley
2018-01-01
|
| Series: | International Journal of Aerospace Engineering |
| Online Access: | http://dx.doi.org/10.1155/2018/1795158 |
| Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
| _version_ | 1832558511274328064 |
|---|---|
| author | Jun Guan Wenjun Yi |
| author_facet | Jun Guan Wenjun Yi |
| author_sort | Jun Guan |
| collection | DOAJ |
| description | The article establishes a seven-degree-of-freedom projectile trajectory model for a new type of spinning projectile. Based on this model, a numerical analysis is performed on the ballistic characteristics of the projectile, and the trajectory of the dual-spinning projectile is filtered with the unscented Kalman filter algorithm, so that the measurement information of projectile onboard equipment is more accurate and more reliable measurement data are provided for the guidance system. The numerical simulation indicates that the dual-spinning projectile is mainly different from the traditional spinning projectile in that a degree of freedom is added in the direction of the axis of the projectile, the forebody of the projectile spins at a low speed or even holds still to improve the control precision of the projectile control system, while the afterbody spins at a high speed maintaining the gyroscopic stability of the projectile. The trajectory filtering performed according to the unscented Kalman filter algorithm can improve the accuracy of measurement data and eliminate the measurement error effectively, so as to obtain more accurate and reliable measurement data. |
| format | Article |
| id | doaj-art-31dae0b1ac6d4fbe97278fafb1a8ad69 |
| institution | Kabale University |
| issn | 1687-5966 1687-5974 |
| language | English |
| publishDate | 2018-01-01 |
| publisher | Wiley |
| record_format | Article |
| series | International Journal of Aerospace Engineering |
| spelling | doaj-art-31dae0b1ac6d4fbe97278fafb1a8ad692025-02-03T01:32:14ZengWileyInternational Journal of Aerospace Engineering1687-59661687-59742018-01-01201810.1155/2018/17951581795158Modeling of Dual-Spinning Projectile with Canard and Trajectory FilteringJun Guan0Wenjun Yi1National Key Laboratory of Transient Physics, Nanjing University of Science and Technology, Nanjing 210094, ChinaNational Key Laboratory of Transient Physics, Nanjing University of Science and Technology, Nanjing 210094, ChinaThe article establishes a seven-degree-of-freedom projectile trajectory model for a new type of spinning projectile. Based on this model, a numerical analysis is performed on the ballistic characteristics of the projectile, and the trajectory of the dual-spinning projectile is filtered with the unscented Kalman filter algorithm, so that the measurement information of projectile onboard equipment is more accurate and more reliable measurement data are provided for the guidance system. The numerical simulation indicates that the dual-spinning projectile is mainly different from the traditional spinning projectile in that a degree of freedom is added in the direction of the axis of the projectile, the forebody of the projectile spins at a low speed or even holds still to improve the control precision of the projectile control system, while the afterbody spins at a high speed maintaining the gyroscopic stability of the projectile. The trajectory filtering performed according to the unscented Kalman filter algorithm can improve the accuracy of measurement data and eliminate the measurement error effectively, so as to obtain more accurate and reliable measurement data.http://dx.doi.org/10.1155/2018/1795158 |
| spellingShingle | Jun Guan Wenjun Yi Modeling of Dual-Spinning Projectile with Canard and Trajectory Filtering International Journal of Aerospace Engineering |
| title | Modeling of Dual-Spinning Projectile with Canard and Trajectory Filtering |
| title_full | Modeling of Dual-Spinning Projectile with Canard and Trajectory Filtering |
| title_fullStr | Modeling of Dual-Spinning Projectile with Canard and Trajectory Filtering |
| title_full_unstemmed | Modeling of Dual-Spinning Projectile with Canard and Trajectory Filtering |
| title_short | Modeling of Dual-Spinning Projectile with Canard and Trajectory Filtering |
| title_sort | modeling of dual spinning projectile with canard and trajectory filtering |
| url | http://dx.doi.org/10.1155/2018/1795158 |
| work_keys_str_mv | AT junguan modelingofdualspinningprojectilewithcanardandtrajectoryfiltering AT wenjunyi modelingofdualspinningprojectilewithcanardandtrajectoryfiltering |